Method of repairing a turbine component

摘要

A method of repairing a turbine component (100) having an array (10) of partitions (12) is provided and includes machining one or more partitions (12) of the array (10) to remove trailing edge sections (124) thereof, fabricating one or more replacement inserts (30), respectively locating the one or more replacement inserts (30) in the one or more machined partitions and substantially simultaneously brazing the one or more replacement inserts (30) to the one or more machined partitions (12).